GB0805577D0 - Acoustic liners - Google Patents
Acoustic linersInfo
- Publication number
- GB0805577D0 GB0805577D0 GBGB0805577.4A GB0805577A GB0805577D0 GB 0805577 D0 GB0805577 D0 GB 0805577D0 GB 0805577 A GB0805577 A GB 0805577A GB 0805577 D0 GB0805577 D0 GB 0805577D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- acoustic liners
- liners
- acoustic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/545—Ducts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/663—Sound attenuation
- F04D29/664—Sound attenuation by means of sound absorbing material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/326—Application in turbines in gas turbines to drive shrouded, low solidity propeller
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/182—Two-dimensional patterned crenellated, notched
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/963—Preventing, counteracting or reducing vibration or noise by Helmholtz resonators
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0805577A GB2458679B (en) | 2008-03-28 | 2008-03-28 | Acoustic liners |
EP09250102.2A EP2105597B1 (en) | 2008-03-28 | 2009-01-15 | Acoustic liner panel for a turbofan engine |
US12/320,268 US7967108B2 (en) | 2008-03-28 | 2009-01-22 | Acoustic liners |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0805577A GB2458679B (en) | 2008-03-28 | 2008-03-28 | Acoustic liners |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0805577D0 true GB0805577D0 (en) | 2008-04-30 |
GB2458679A GB2458679A (en) | 2009-09-30 |
GB2458679B GB2458679B (en) | 2010-04-21 |
Family
ID=39386851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0805577A Expired - Fee Related GB2458679B (en) | 2008-03-28 | 2008-03-28 | Acoustic liners |
Country Status (3)
Country | Link |
---|---|
US (1) | US7967108B2 (en) |
EP (1) | EP2105597B1 (en) |
GB (1) | GB2458679B (en) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2963469B1 (en) | 2010-07-27 | 2012-07-27 | Aircelle Sa | ACOUSTIC PANEL |
FR2971613B1 (en) * | 2011-02-10 | 2013-03-15 | Airbus Operations Sas | PANEL FOR ACOUSTIC PROCESSING COMPRISING JOINT BETWEEN TWO PARTS AND METHOD OF REPAIRING A PANEL FOR ACOUSTIC TREATMENT |
US8695915B1 (en) * | 2011-03-11 | 2014-04-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Flap side edge liners for airframe noise reduction |
US9227719B2 (en) | 2011-03-11 | 2016-01-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Reactive orthotropic lattice diffuser for noise reduction |
WO2012145141A1 (en) | 2011-04-20 | 2012-10-26 | Dresser-Rand Company | Multi-degree of freedom resonator array |
US8596413B2 (en) * | 2011-07-25 | 2013-12-03 | Dresser-Rand Company | Acoustic array of polymer material |
FR2984280B1 (en) * | 2011-12-15 | 2013-12-20 | Aircelle Sa | AIR INTAKE STRUCTURE FOR TURBOREACTOR NACELLE |
FR2999650B1 (en) * | 2012-12-17 | 2018-07-13 | Safran Aircraft Engines | REMOVABLE ACOUSTIC PANELS FOR TURBOREACTOR HOUSING. |
US10094242B2 (en) | 2014-02-25 | 2018-10-09 | United Technologies Corporation | Repair or remanufacture of liner panels for a gas turbine engine |
GB201405496D0 (en) | 2014-03-27 | 2014-05-14 | Rolls Royce Plc | Linear assembly |
FR3058672B1 (en) * | 2016-11-14 | 2019-05-10 | Safran | THRUST REVERSING SHUTTER, AND METHOD OF MANUFACTURING |
US10612564B2 (en) | 2017-03-07 | 2020-04-07 | Rolls-Royce Corporation | Acoustic panel of turbine engine and method of arranging the acoustic panel |
US10473030B2 (en) * | 2017-03-07 | 2019-11-12 | Rolls-Royce Corporation | Acoustic panel of turbine engine |
US11059559B2 (en) | 2018-03-05 | 2021-07-13 | General Electric Company | Acoustic liners with oblique cellular structures |
US10823059B2 (en) * | 2018-10-03 | 2020-11-03 | General Electric Company | Acoustic core assemblies with mechanically joined acoustic core segments, and methods of mechanically joining acoustic core segments |
US11434819B2 (en) | 2019-03-29 | 2022-09-06 | General Electric Company | Acoustic liners with enhanced acoustic absorption and reduced drag characteristics |
US11352953B2 (en) | 2019-04-05 | 2022-06-07 | Rolls-Royce Corporation | Acoustic panel with reinforced lip |
US11313324B2 (en) * | 2019-04-12 | 2022-04-26 | Rolls-Royce Corporation | Systems and methods of acoustic dampening in a gas turbine engine |
US11260641B2 (en) | 2019-05-10 | 2022-03-01 | American Honda Motor Co., Inc. | Apparatus for reticulation of adhesive and methods of use thereof |
CN110487533B (en) * | 2019-09-17 | 2021-11-19 | 中国航发沈阳发动机研究所 | Sound lining test piece, assembling method and test structure thereof |
US11668236B2 (en) | 2020-07-24 | 2023-06-06 | General Electric Company | Acoustic liners with low-frequency sound wave attenuating features |
US20220099121A1 (en) * | 2020-09-25 | 2022-03-31 | Caterpillar Inc. | Panel assembly and aftertreatment assembly including panel assembly |
US11460048B2 (en) * | 2020-12-18 | 2022-10-04 | Rohr, Inc. | Attachable acoustic panels and method of making same |
US11970992B2 (en) | 2021-06-03 | 2024-04-30 | General Electric Company | Acoustic cores and tools and methods for forming the same |
US11680524B1 (en) | 2021-12-16 | 2023-06-20 | Rolls-Royce Corporation | Turbine engine acoustic panel with outer flange case mounting |
US11946414B2 (en) | 2021-12-16 | 2024-04-02 | Rolls-Royce Corporation | Manufacture methods and apparatus for turbine engine acoustic panels |
US11591927B1 (en) | 2021-12-16 | 2023-02-28 | Rolls-Royce Corporation | Turbine engine fan track liner with outer flange case mounting |
US11965425B2 (en) | 2022-05-31 | 2024-04-23 | General Electric Company | Airfoil for a turbofan engine |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4161231A (en) * | 1973-10-31 | 1979-07-17 | Rolls-Royce Limited | Metal cavitated sandwich structures |
DE19804718C2 (en) * | 1998-02-06 | 2001-09-13 | Eurocopter Deutschland | Sound absorbing sandwich wall |
US6182787B1 (en) * | 1999-01-12 | 2001-02-06 | General Electric Company | Rigid sandwich panel acoustic treatment |
US6256959B1 (en) * | 1999-10-14 | 2001-07-10 | Kjmm, Inc. | Building panel with vibration dampening core |
JP3584465B2 (en) * | 1999-11-11 | 2004-11-04 | 日産自動車株式会社 | Sound absorbing structure |
GB0119608D0 (en) | 2001-08-11 | 2001-10-03 | Rolls Royce Plc | A guide vane assembly |
FR2840647B1 (en) * | 2002-06-05 | 2004-10-29 | Airbus France | DEVICE FOR CONNECTING TWO TUBULAR PIECES OF AIRCRAFT TURBOREACTOR |
FR2844304B1 (en) * | 2002-09-10 | 2004-12-10 | Airbus France | ACOUSTICALLY RESISTIVE LAYER FOR ACOUSTIC MITIGATION PANEL, PANEL USING SUCH A LAYER |
FR2856379B1 (en) * | 2003-06-18 | 2006-11-24 | Airbus France | AIRCRAFT ENGINE HAVING BLOWER HOUSINGS AND THRUST INVERTERS SEPARATED BY REDUCED GAME |
GB2418957B (en) * | 2003-10-22 | 2006-07-05 | Rolls Royce Plc | A liner for a gas turbine engine casing |
GB2407343B (en) * | 2003-10-22 | 2006-04-19 | Rolls Royce Plc | An acoustic liner for a gas turbine engine casing |
US7328771B2 (en) * | 2004-07-27 | 2008-02-12 | United Technologies Corporation | Zero acoustic splice fan case liner |
US7296656B2 (en) * | 2005-04-22 | 2007-11-20 | United Technologies Corporation | Acoustic mechanical retainer |
US7296655B2 (en) * | 2005-04-22 | 2007-11-20 | United Technologies Corporation | Duct liner acoustic splice |
US20080086965A1 (en) * | 2006-10-16 | 2008-04-17 | Metz Timothy W | Composite structural panel |
US20090078820A1 (en) * | 2007-09-26 | 2009-03-26 | The Boeing Company | Wing-to-body fairing |
FR2926614B1 (en) * | 2008-01-23 | 2010-02-12 | Aircelle Sa | METHOD FOR JOINING ACOUSTIC ALVEOLAR PANELS |
-
2008
- 2008-03-28 GB GB0805577A patent/GB2458679B/en not_active Expired - Fee Related
-
2009
- 2009-01-15 EP EP09250102.2A patent/EP2105597B1/en not_active Not-in-force
- 2009-01-22 US US12/320,268 patent/US7967108B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP2105597A2 (en) | 2009-09-30 |
EP2105597A3 (en) | 2015-03-04 |
US20090242321A1 (en) | 2009-10-01 |
GB2458679A (en) | 2009-09-30 |
EP2105597B1 (en) | 2016-03-23 |
GB2458679B (en) | 2010-04-21 |
US7967108B2 (en) | 2011-06-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20220328 |